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WO/2022/055795A1 |
Disclosed are devices, systems, apparatus, methods, products, and other implementations, including a method for detecting damage in a geographical area that includes receiving a first image of the geographical area, with the first image ...
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WO/2022/055673A1 |
Mining apparatuses, systems, and methods related to using a rocket engine's plume and a collection manifold to efficiently displace, collect, process, and store frozen volatiles embedded within or below a surface are disclosed. The plume...
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WO/2022/053768A1 |
The invention relates to a method for manufacturing an aerospace and/or aeronautic tubular composite part (1), said tubular composite part (1) comprising a tubular body (10) and at least one flange (22). The method comprising the followi...
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WO/2022/049332A1 |
The invention relates to a telescopic mast (100) comprising: • - coaxial segments (101_1,..., 101_N) that can be controlled from a stowed position to a deployed position, • - a set of guide systems (104, 104P) arranged between the ad...
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WO/2022/051511A1 |
A spacecraft propulsion system comprises an attitude adjustment thruster system with multiple thrusters (488a-d) receiving heated propellant via a shared thermal capacitance block (275). The thermal capacitance block (275) with integrate...
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WO/2022/047551A1 |
(57) This invention relates to a system for deploying solar panels for nanosatellites, which will find application in science, in space research, and in particular in the equipment of nanosatellites of the CubeSats type. The developed sy...
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WO/2022/049524A1 |
The planar electric motor for aerospatial use is a 100% electrical drive, consisting of a device capable of generating a thrust force on itself, regardless of the environment surrounding the same, even in a vacuum or in outer space. The ...
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WO/2022/051513A1 |
A spacecraft propulsion system comprises an attitude adjustment thruster system with multiple thrusters (488a-d) receiving heated propellant via a shared thermal capacitance block (275). The thermal capacitance block (275) receives energ...
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WO/2022/044007A1 |
The invention is an implementation of the space elevator wherein an inflatable tube is held up by the force of wind rushing through it from surface to height, in the manner of the 'inflatable dancer' used for advertisments. Since the dev...
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WO/2022/046103A1 |
Electro spray devices and methods of fabricating electro spray devices are described
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WO/2021/058356A9 |
The invention relates to an aerial transport device by means of connections with supply lines and cables for the transport of electricity, liquids and goods, at the limit of the atmospheres of the planets, in areas with low gravitational...
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WO/2022/040024A1 |
A wireless anti-static device is disclosed, including an electronic sensing circuit that measures the polarity and electrostatic potential of the subject relative to its surroundings. Ion guns of positive and negative polarities are able...
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WO/2022/039782A1 |
A missile including an upper stage and at least one lower stage is provided. The upper stage includes a primary flight computer configured to control a flight of the upper stage along a missile flight path such that, for example, it reac...
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WO/2022/040329A1 |
A propulsion method including the steps of providing a vehicle comprising a cylindrical reactor unit; conducting a nuclear fusion reaction in the cylindrical reactor unit; and deflecting a pulse of electrically charged ions from the cyli...
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WO/2022/040653A1 |
An unmanned aerial vehicle (UAV) or "drone" executes a neural network to assist with inspection, surveillance, reporting, and other missions. The drone inspection neural network may monitor, in real time, the data stream from a plurality...
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WO/2022/040146A1 |
Embodiments of the present disclosure generally relate to methods for cleaning aerospace components having oxidation, corrosion, contaminants, and/or other degradations. In one or more embodiments, a cleaning method includes positioning ...
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WO/2022/036276A1 |
A deployable electromagnetic radiation antenna system for extraterrestrial deployment of an electromagnetic radiation directing surface, the deployable electromagnetic radiation antenna system comprising is provided. The deployable elect...
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WO/2022/032370A1 |
An artificial orbital ring system (AORS) is configured in the form of a ring-shaped satellite (1) placed on a circular orbit (5) at a height Ho around a natural astronomical body (2) in the plane (3) of the equator (4). The system compri...
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WO/2022/029827A1 |
An extensible mast (1) according to the present invention is characterized by being provided with a first fiber layer (2) which uses a fiber-reinforced plastic, a second fiber layer (3) which is disposed in contact with the first fiber l...
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WO/2021/225655A9 |
A multi-user satellite system provides communication services to external satellites. This satellite system provides in-orbit access points that can be used by the external satellites to offload data instead on relying directly on ground...
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WO/2022/026032A1 |
A flexible solar array for extraterrestrial deployment and a method of manufacturing such a flexible solar array are disclosed. A power generating layer, a durable layer, and an ultraviolet radiation blocking layer are disposed such that...
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WO/2022/020382A1 |
A magnetohydrodynamic pump for use in pumping molten salts that improves upon existing solutions is disclosed. The magnetohydrodynamic pump utilizes a linear induction motor with a cavity lined with ceramic and an interior piece forcing ...
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WO/2022/016243A1 |
The present invention relates to a system for obtaining a compound for blocking cosmic, nuclear and electromagnetic radiation, comprising a hydrogen reservoir (110), a hydrocarbon reservoir (120), a vacuum chamber (130), a spark power so...
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WO/2022/018381A1 |
Disclosed is a method and system for detecting a target in space, based on images taken from a spacecraft such as a visual inspection satellite. The invention relates to a method for remotely detecting one or more targets (1) in space in...
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WO/2022/014694A1 |
The present invention provides a method of controlling a horizontal translational motion of a rocket without changing the posture of an aircraft and without increasing manufacturing costs or operating costs, to thus accurately execute a ...
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WO/2022/014209A1 |
[Problem] To provide an optical device which makes it possible to variously change the direction in which the radiation pressure of light acts. [Solution] This optical device extends along a reference plane, and is provided with a plural...
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WO/2022/011078A1 |
A telescope apparatus includes a telescope array comprising a plurality of telescopes each having a telescope aperture configured to receive light from a respective field of view. A light sensor is associated with each telescope to recei...
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WO/2022/010485A1 |
A spacecraft propulsion system including a first thruster system including a first power processing unit (30) connected to a first thruster string (20) via a crossover switching unit (40) and connected to a second thruster string (20) vi...
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WO/2022/008386A1 |
Disclosed is a primary structure (100) for a spacecraft (200), comprising an interface ring (10) and a predetermined number of panels defining a box arranged so as to close an interior volume of the spacecraft, the box being connected to...
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WO/2022/010819A1 |
A satellite used in a multi-satellite LEO/VLEO constellation is configured to reduce drag and increase satellite life in orbit by virtue of its streamlined casing. The satellite has a longitudinal axis defining the y-axis of a right-hand...
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WO/2022/004040A1 |
A system for controlling an operation of a vehicle to rendezvous with a target over a finite time horizon, wherein the vehicle and the target form a multi- object celestial system. A processor to formulate passive unsafe regions as passi...
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WO/2022/003284A1 |
The present invention relates to a method (50) for orbit control of a satellite (10) orbiting Earth and desaturation of a device for storing kinematic momentum of the satellite, the satellite (10) comprising two articulated arms (20, 21)...
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WO/2022/004044A1 |
Systems and methods controlling an operation of a vehicle in real time to rendezvous the vehicle with a target over a finite time horizon having multiple specified time periods. Select a set of unsafe regions from stored unsafe regions, ...
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WO/2021/262867A1 |
A method for orbital collision screening comprising, obtaining trajectory information of a plurality of objects moving on predictable paths. For each one of the plurality of objects, based upon respective trajectory information of the on...
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WO/2021/254547A1 |
A supporting structure for vertical transport comprising an anchoring segment mounted on the ground, a trunk of passive and compensation segments that are provided with containers with a lifting gas, wherein the lifting power of the lift...
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WO/2021/258060A1 |
A closed-loop, bioregenerative water purification system including a gravity-independent anaerobic membrane bioreactor capable of operating in the presence and absence of gravity, the bioreactor including an anaerobic bioreactor, a first...
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WO/2021/255444A2 |
A device for protecting a body from damage. The protective device comprises an outer protective cover, the outer protective cover comprising a thermal energy conduction element for transferring thermal energy through at least part of the...
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WO/2021/257002A1 |
The subject-matter of invention is a spacecraft powered by electromagnetic waves with a primary and secondary tunnel for acceleration in the interplanetary, interstellar and intergalactic space and generation of electricity to power the ...
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WO/2021/255920A1 |
The present invention enables an image-capturing plan in which changes have been reflected to be swiftly created. An image-capturing plan creating device according to the present invention comprises: an image-capturing plan creating unit...
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WO/2021/242302A1 |
Systems, methods, devices, and non-transitory media of the various embodiments may enable the identification of launch opportunities. The integrated approach of the various embodiments leverages instrumentation, data and communication sy...
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WO/2021/240487A1 |
The invention relates to a method (100) for adjusting the path of a satellite (10) to limit a risk of collision with items of debris (d1, di) each having a date of closest pass (TCA1, TCAi) with the satellite (10), the method (100) compr...
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WO/2021/243244A1 |
A nuclear fuel assembly for a nuclear reactor core, the fuel assembly having at least one fuel element including an elongated shell defining an interior volume, a lattice structure disposed within the interior volume, at least one flow c...
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WO/2021/241365A1 |
This space debris orbit changing method comprises: a step for observing space debris floating in outer space; and a step for irradiating the observed space debris with solar light condensed by an irradiation satellite provided in outer s...
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WO/2021/240404A1 |
A release system (1) for the release of satellites from a launch vehicle comprising: (i) a torsion bar (2), having a first end (2a) which is fixed by means of support means (4) to a launch vehicle (3) and is locked in rotation around a l...
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WO/2021/239732A1 |
The invention relates to a method (100) for estimating collision between a satellite (10) in orbit and at least one piece of space debris (d1) having a time of closest approach (TCA)) to the satellite (10), the method (100) comprising th...
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WO/2021/235487A1 |
Provided is a space debris removal method comprising a step for putting, on a ballistic trajectory, a space debris removal device capable of spraying liquid hydrogen or an ionic liquid, and a step for spraying the liquid hydrogen or the ...
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WO/2021/234246A1 |
The invention proposes a device (1) for deploying and pointing an item of equipment, comprising: - a mobile platform (20) for receiving the item of equipment, - a carrier (10) rigidly attached to a wall of a spacecraft, and - three ident...
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WO/2021/234054A1 |
The invention relates to a method for transferring a spacecraft (10), such as an artificial satellite, from an initial elliptical orbit (30) to a final geostationary orbit (50), said spacecraft taking at least one intermediate elliptical...
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WO/2021/229178A1 |
The invention relates to a deployment device (1) for a nano-satellite (5) comprising a main structure (2) mounted on a launcher, a support frame (3) carrying the nano-satellite (5), a locking/unlocking structure (4), the deployment devic...
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WO/2021/230170A1 |
A database (102) of a rocket launch assistance device stores orbital prediction information about a satellite megaconstellation (301) acquired from a space information recorder provided in a megaconstellation operations device, and space...
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